CZ-4B R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite CZ-4B R/B at a glance.

Uptime

8090

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.7

Latest

Satellite identification and parameters

Extended collection of information and parameters for CZ-4B R/B.

Object identification

Identified? True

Debris? False

Object name: CZ-4B R/B

International designator: 2003-049C

Object number (NORAD): 28059

Object ID (CCSDS): 28059

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 98.975 minutes

Inclination: 98.6789 deg

SMA: 7087.798 km

Apoapsis: 744.377 km

Periapsis: 674.949 km

RAAN: 332.7972 deg

Eccentricy: 0.00489773

Argument of periapsis: 137.5506 deg

Mean anomaly: 222.9494 deg

Mean motion: 14.54908751 rev/day

Mean motion (dot): 0.00000644 rev/day2

B* drag term: 0.00015920703 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 10:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 12, 2025, 6:02 a.m. UTC

TLE line 0: 0 CZ-4B R/B

TLE line 1: 1 28059U 03049C 25346.25175911 .00000644 00000-0 15921-3 0 9996

TLE line 2: 2 28059 98.6789 332.7972 0048977 137.5506 222.9494 14.54908751173881

Live tracking on map

Real-time ground track for satellite CZ-4B R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object CZ-4B R/B.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB SSO 2025-06-15 03:15:42 0.0001527408 425.0 (m) DEBRIS
DELTA 1 DEB SSO 2024-12-13 21:49:29 0.0004283221 346.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-09 04:43:45 0.0001446308 475.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-07-22 20:46:19 0.0001486641 287.0 (m) DEBRIS

Associated space launch

The satellite is China's first operational civilian remote-sensing satellite, specifically designed for the Chinese Ministry of Land and Resources (MLR).

CZ-4B R/B was lifted into orbit during the mission ‘Long March 4B | Zi Yuan 1-2’, on board a Long March 4B space rocket.

The launch took place on Oct. 21, 2003, 3:16 a.m. from Launch Complex 7.

For more information about the launch, click the button.

Launch to space Long March 4B | Zi Yuan 1-2
Long March 4B | Zi Yuan 1-2

Agency: N/A

Status: Launch Successful

Launch date: Oct. 21, 2003, 3:16 a.m. UTC

Rocket: Long March 4B

Launch pad: Launch Complex 7

Location: Taiyuan Satellite Launch Center, People's Republic of China

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